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| Description | Parameters | Notes |
| Maximum / Average cruising speed | 90/65?Km/h? | Manual flight |
| Maximum Flying Height | 2500?m? | Manual flight |
| Rate of Climb | 4?m/s? | <4KG payload,manual flight |
| Net Weight | 16.35?Kg? | Including the main rotor, without shell |
| Take-off Weight | 35?Kg? | Including standard fuel and Flight Control Units |
| Maximum payload | 13?Kg? | |
| Standard Fuel Tank | 2.5 X 2?L? | Extensible |
| Maximum Airborne Period | 1?H? | Extensible |
| Diameter of Main Rotor/Tail Rotor | 2146/403?mm? | Material: carbon fiber |
| Gasoline Engine | 80CC | Air-cooled double opposed cylinder |
| Fuel | 93.97?Octane? | gasoline fuel (Mixing ratio 1:25) |
| Fuel Consumption | 4000?cc/h? | Mean (90% load) |
| Start-up Mode | Motor and Battery | External dedicated starter |
| Gear Ratio | 5.84/1/4.69 | Engine / Main rotor / Tail rotor |
| Battery Duration | 2?hrs? | Continuous work (Without generators) |
| Three Axis Camera Mount | 3-axis remote control | Video return and horizon gyroscope can be installed |
| Flight Control Stability Augmentation System | 3-axis gyroscope, 3 axis accelerometer 3 axis magnetic compass sensors, GPS navigation, stability increasing manipulation |
| Temperature Range | -20+50??? | Standard version |
| Total length of the aircraft | 2630/711?mm? | Main rotor blade side/Tail rotor blade side |
| Transport Box size | 1.3 X 0.5 X 0.7?m? | Packed double cardboard boxes of about 40 kg |
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